Effect of Incoming Boundary Layer on Supersonic Mixing Layer Generated by Wall-Mounted Ramp Injector
19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
01.01.2014
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2014
|Supersonic Boundary-Layer Combustion via Multiporthole Injector Arrays
Online Contents | 2015
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